23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5579742015361007---------------------------
|
|
|
|
Spacecraft: mySat
|
|
dry_mass: 200.0 kg
|
|
specific impulse: 3200.0 kg/s
|
|
max_thrust: 0.00025 kN
|
|
num_thrusters: 1
|
|
duty_cycle: 1.0
|
|
Launch Mass: 3500.0 kg
|
|
Launch Date: 2024-05-11T18:37:35.300
|
|
Launch V∞: [7.829809881888154, -5.8507855700338345, 0.073588755543928] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [-2.5201093600753834e-5, -2.1262999434174632e-5, -0.0013355275009632002] km/s
|
|
V∞_out: [0.001257005586654514, 0.0004282710045048528, -0.0001958345988389249] km/s
|
|
time of flight: 1.811297817544177e8 seconds
|
|
arrival date: 2030-02-06T04:27:16.300
|
|
thrust profile: [0.3671885077599352 -0.007893791718822452 -0.11299040622469989; 0.08534807197560375 0.047723464422800975 -0.09211524696319802; 0.09941730718657477 0.09524973324633973 -0.19031295953561483; 0.03777697274013195 0.04604714524904377 -0.10763443993550817; 0.029838818922420234 0.04526890719024147 -0.11515296984025494; 0.011998211988378745 0.021024741566674828 -0.05990126114186747; 0.015416947404296416 0.0325370317251882 -0.09544505853711574; 0.006679200833244801 0.015321774080593922 -0.049381606020669835; 0.0038887595173968705 0.009825016166720815 -0.033849444800789184; 0.0017445883785681248 0.004939327891312054 -0.017504910056123237; -1.6223180076900112e-6 0.0013803236589063656 -0.004927156235065043; 0.0003099522041489243 0.0010015069651862242 -0.0038551299693012566; -0.001143448603303661 0.0006073706805987772 -0.002374340206506656; -2.1189993293921957e-7 0.00027697390710757267 -0.0008060360013689304; 0.00025390543600888613 -0.00010927166008004702 -0.0008128717064740587; -0.0009883250452407994 -0.0004447006336932192 0.0007793624838475525; 0.0009437745069618845 0.001911708602089676 -0.000738668566704281; 0.0010100405531664194 -0.0018095513891301053 -0.0022264992543374407; 5.972932917698052e-5 3.2317496751725335e-5 -0.00015482138247914956; 0.00017641372850097167 0.001392848748459323 0.0008738951838149914] %
|
|
|
|
Mass Used: 93.63556083728054 kg
|
|
Launch C3: 95.54302987797203 km²/s²
|
|
||V∞_in||: 0.0013359344729786046 km/s
|